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针栓式喷嘴喷雾燃烧特性研究进展
引用本文:谢远,聂万胜,姜传金,罗修棋,仝毅恒.针栓式喷嘴喷雾燃烧特性研究进展[J].推进技术,2022,43(7):42-60.
作者姓名:谢远  聂万胜  姜传金  罗修棋  仝毅恒
作者单位:航天工程大学,航天工程大学,航天工程大学,航天工程大学,航天工程大学
基金项目:国家自然科学基金(12002386)。
摘    要:针栓式喷嘴具有深度节流、结构简单、燃烧稳定等优点,主要用于变推力液体火箭发动机。本文首先介绍针栓式喷嘴的工作原理和发展历程,紧接着总结针栓式喷嘴的雾化特性和燃烧特性,最后展望针栓式喷嘴未来的研究方向。目前针栓式喷嘴的雾化特性研究较多,重点分析了工况参数和结构尺寸对破碎形态、喷雾锥角、SMD、液滴速度等的影响,针对针栓式喷嘴液膜破碎机理的研究相对较少;针栓式喷嘴燃烧特性研究主要集中于燃烧流场结构、燃烧性能和热防护等方面,对针栓式发动机固有燃烧稳定性机理以及动态燃烧特性的研究还较为欠缺。

关 键 词:针栓式喷嘴  雾化  燃烧  变推力液体火箭发动机
收稿时间:2021/6/4 0:00:00
修稿时间:2022/6/9 0:00:00

Research Progress on Spray Combustion Characteristics of Pintle Injector
XIE Yuan,NIE Wan-sheng,JIANG Chuan-jin,LUO Xiu-qi,TONG Yi-heng.Research Progress on Spray Combustion Characteristics of Pintle Injector[J].Journal of Propulsion Technology,2022,43(7):42-60.
Authors:XIE Yuan  NIE Wan-sheng  JIANG Chuan-jin  LUO Xiu-qi  TONG Yi-heng
Institution:University of Aerospace Engineering,,,,University of Aerospace Engineering
Abstract:The pintle injector has the advantages of deep throttling, simple structure and stable combustion, etc. It is mainly used in variable thrust liquid rocket engine. In this review, the working principle and development history of the pintle injector are introduced firstly, then the atomization and combustion characteristics of the pintle injector are summarized, and finally the future research direction of the pintle injector is prospected. At present, there are many studies on the atomization characteristics of the pintle injector, focusing on the analysis of the effects of working conditions and structure size on the crushing morphology, spray cone Angle, SMD and droplet velocity, etc., but the research on the liquid film breaking mechanism of the pintle injector is relatively few. The research on the combustion characteristics of the pintle mainly focuses on the structure of combustion flow field, combustion performance and thermal protection, etc. However, the research on the mechanism of the inherent combustion stability and dynamic combustion characteristics of the pintle-type engine is still relatively lacking.
Keywords:Pintle injector  Atomization  combustion  Variable thrust liquid rocket engine
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